JASC 7220
Service difficulty reports · 1,719
Reports filed under 7220 · Turbine Engine Air Inlet Section, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7220' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7220' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR NACA2021061100001Blade · dentedDISCREPANCY: REF. DMI 72-31 RIGHT ENGINE BLADE #16 DENTED. CORRECTIVE ACTION: PERFORMED NDT SPOT FLUORESCENT PENETRANT INSPECTION #16 BLADE LE NO CRACK INDICATION NOTED.SDR NACA2021061000006Blade · dentedDISCREPANCY: RIGHT ENGINE #16 DENTED. CORRECTIVE ACTION: BLENDED R ENGINE BLADE #16 FOUND WITHIN LIMITS PER AMM 72-31-02SDR ASAA2021052734986Flange · damaged#1 ENGINE MAINT CODE 76-21361, THE START LEVER SIGNALS DISAGREE, LONG TIME FAULT, DEF PER T/C 78273000. GROUNDED - YES. REF T/C # 78471000 #1 ENGINE ESN 894832 REMOVED FOR OTHER CAUSE (OIL INLET COVER ATTACH FLANGE DAMAGE) REF LOGPAGE 60181836SDR ASAA2021052734988Flange · damaged#1 ENGINE MAINT CODE 76-11361, THE START LEVER SIGNALS DISAGREE, LONG TIME FAULT, DEF PER T/C 78273000. GROUNDED - YES. #1 ENGINE REMOVED FOR OTHER CAUSE, OIL INLET COVER ATTACH FLANGE DAMAGE.SDR UIEA2021052301165Blades · dentedFOUND LEADING EDGE FAN BLADES ON #1 ENGINE BLADES 4, 6, 7, 13, 15, 16, 29, 34, & 36 TO HAVE MINOR DENTS.(<P>INSPECTED FAN BLADES IAW B767 AMM 72-31-02. ALL BLADES FOUND TO BE WITHIN AMM LIMITS FOR SERVICE. NO OTHER ACTION NECESSARY. TRANSFERRED TO NON-MEL # 14SDR ASAA2021051634823Spacer · debondedPER T/C 78472010 #2 ENG BLADE LUBE SPACERS #4,6,7,10,14,15,16, 18, 19 AND 24 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REPLACED SPACERS AT POSITION 4,6,7,10,14,15,16,18,19, AND 24 PER T/C 78472010. NO DEFECTS NOTED.SDR ASAA2021051434822Pin · damagedWHILE ACCOMPLISHING T.C. SB CFM56-7B-72-0986-1 FOUND 3RD STG VSV SLAB HEAD PIN LIBERATED @ 3 O'CLOCK POSITION ALF CAUSING DAMAGE TO BOOSTER SPOOL ALONG WITH DOWNSTREAM HPC BLADE DAMAGE. #2 POSN. ESN 805120. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE REF TCSDR ASAA2021051034783Spacer · wornSPACERS AT POSITIONS 1, 2, 3, 4, 5, 7, 10, AND 13 REQUIRE REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED SPACERS AT POSITIONS 1, 2, 3, 4, 5, 7, 10, AND 13. REF TC 78472010.SDR ASAA2021050434748Blade · misinstalledPER T/C 78472010 #1 ENG FAN BLADE LUBE PLATFORMS #3, 18, 19, AND 24 P/N 340-001-816-0 ARE NOT PAIRED 180 DEGREES. GROUNDED - YES. REMOVED AND REPLACED PLATFORMS #3,18,19, AND 24 WITH PN 340-001-817-0 PER T/C 78472010 ARE NOW PAIRED 180 DEGREES.SDR ASAA2021050134730Spacer · defectiveREF TC 78472010, SPACERS ON #1 ENGINE BAD SPACERS #9 AND #10. GROUNDED - YES. REMOVED AND REPLACED #9 AND #10 SPACERS FROM #1 ENGINE REF TC 78472010.SDR ASAA2021043034729Spinner · wornREF T/C 78472000 #2 ENG FRONT SPINNER CONE ANODIZED COATING AND WHITE ANTI-EROSION PAINT WORN TO LIMITS. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FRONT SPINNER CONE REF B737-800 AMM 72-21-01.SDR ASAA2021042834693Spacer · debondedPER T/C 78472010 #2 ENG. FAN BLADE LUBE SPACERS #3,4,8,9,10,11,12,14,16,21 ARE DISBONDED. GROUNDED - YES. REPLACED SPACERS #3,4,8,9,10,11,14,16 AND 21 REF T/C 78472010.SDR ASAA2021042734700Blade · wornPER T/C 78472010 #2 ENG FAN BLADE LUBE #15 PLATFORM ELASTOMER SEAL IS WORN. GROUNDED - YES. REMOVED AND REPLACED #15 PLATFORM PER T/C 78472010.SDR ASAA2021042734699Spacer · debondedPER T/C 78472010 #2 ENG. FAN BLADE LUBE SPACERS #1,7,8,10,14,18,22 AND 24 ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FAN BLADE SPACERS #1,7,8,10,14,18,22 AND 24 PER T/C 78472010.SDR ASAA2021042734697Spinner · nickedPER T/C 78472010 #2 ENG FAN BLADE LUBE REAR CONE HAS A NICK BETWEEN BALANCE SCREWS #20 AND 21 11747 04/26/2010. GROUNDED - YES. REMOVED REAR TAIL CONE AND INSTALLED ALL NOMINAL BALANCE WEIGHTS REF B737-800 AMM 71-00-250-802-F00. INSTALLED REAR CONE PER T/C 784SDR ASAA2021042734695Blade · wornPER T/C 78472010 #2 ENG FAN BLADE LUBE #4 BLADE CU-NI-IN COATING MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #4 FAN BLADE SET ON #2 ENGINE PER T/C 78472010.SDR ASAA2021042634701Blade · wornPER T/C 78472010 #2 ENG FAN BLADE LUBE #7 BLADE CU-NI-IN COATING MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #7 FAN BLADE PER T/C 78472010.SDR ASAA2021042634698Blade · damagedPER T/C 78472010 #2 ENG FAN BLADE LUBE #24 PLATFORM AFT BUSHING SURFACE HAS GOUGE. GROUNDED - YES. REMOVED AND REPLACED #24 PLATFORM PER T/C 78472010.SDR ASAA2021042634696Blade · wornPER T/C 78472010 #2 ENG FAN BLADE LUBE #14 BLADE CU-NI-IN MISSING COATING BEYOND LIMITS. GROUNDED - YES. RMVD & REPLACED #14 FAN BLADE SET ON #2 ENG PER T/C 78472010.SDR ASAA2021042634673Spacer · debondedWHILE ACCOMPLISHING MTC 78472010, FOUND #2 ENG #7 & #22 FAN BLADE SPACER WITH DISBONDED ELASTOMERS. GROUNDED - YES. REPLACED #2 ENG #7 AND #22 FAN BLADE SPACERS REF T/C 78472010.SDR ASAA2021042534662Spacer · debondedPER T/C 78472010 #1 ENG FAN BLADE LUBE SPACERS #18 & 24 ELASTOMERS ARE DISBONDED. GROUNDED - YES. INSTALLED NEW SPACERS #18 & 24 PER TASKCARD 78472010.SDR ASAA2021042534661Screw · unsecure#1 ENGINE SPINNER REAR CONE BALANCE SCREWS REQUIRE TORQUE. GROUNDED - YES. TORQUED #1 ENG REAR SPINNER CONE BALANCE SCREWS REF TASKCARD 78472010.SDR ASAA2021042534660Panel · loosePER T/C 78472000 #1 INLET INSP FAN DUCT PANEL #8 IS LOOSE. GROUNDED - YES. RETIGHTENED FASTENERS FOR #8 FAN DUCT PANEL #1 ENG REF B737-800 AMM 75-23-07.SDR ASAA2021042534659Nut Plate · wornPER T/C 78472010 #1 ENG FAN BLADE LUBE REAR CONE NUTPLATE IS WORN. GROUNDED - YES. REPLACED #1 ENG REAR CONE REF TASCARD 78472010.SDR FDEA202104210964Flange · corrodedNR 2 ENGINE HAS SIGNS OF CORROSION ON FAN CASE FWD FLANGE FROM APPROXIMATELY 4 TO 8 O'CLOCK POS. REFERENCE NONROUTINE N00018 WORK ORDER 79912 ITEM FOUND DURING B-CHECK. CORROSION IS MORE THAN 10 INCHES IN CUMULATIVE CIRCUMFERENCE. CIRCUMFERENCE. REF N1SDR 2021F00124Blade · damagedUNDERCOAT MISSING ON CONCAVE SIDE OF RIGHT ENGINE FAN BLADE DURING OVERNIGHT AND APPLICATION OF 1000 F WING INSPECTION AT MEX, IT WAS DETECTED UNDERCOAT MISSING ON CONCAVE SIDE OF RIGHT ENGINE FAN BLADE. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING TWSDR ASAA2021041934620Blade · erodedWHILE ACCOMPLISHING MTC 78472010, FOUND NR 2 ENG FAN BLADE NR 13 WITH MISSING CU-NI-IM COATING. MISSING BEYOND ALLOWABLE LIMITS. 27MM ON THE CONCAVE SIDE CONTACT AREA. GROUNDED - YES. REPLACED NR 13 FAN BLADE ON NR 2 ENG. AND ITS PAIR NR 1 PER T/C 78472010.SDR ASAA2021041734596Blade · wornWHILE ACCOMPLISHING FAN LUBE ON #2 ENG T/C #78472010 FOUND #13 BLADE WITH MISSING CUNI COATING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #13 FAN BLADE ON #2 ENG IAW ASA MTX TASKCARD #78472010.SDR ASAA2021041434576Platform · wrong partPER T/C 78472010 #2 ENG FAN BLADE LUBE INSP, PLATFORM #11 HAS A WRONG PART #. GROUNDED - YES. REPLACED #11 PLATFORM ON #2 ENGINE PER T/C 78472010.SDR ASAA2021041434575Spacer · debondedPER T/C 78472010 #2 ENG FAN BLADE LUBE INSP SPACERS #4 AND 16 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REPLACED #2 ENG BLADE SPACERS #4 AND #16 PER T/C 78472010.SDR AALA202104119009Engine · inoperativeAIRCRAFT WAS GROUNDED: CLIMBING THRU FL340 ENCOUNTERED SIGNIFICANT AIRFRAME VIBRATION FOLLOWED BY ODOR IN THE COCKPIT AND CABIN. ENGINE #2 N1 AND N2 ERATIC WITH LOSS OF THRUST AND HIGH ENGINE VIBRATION. SECURED ENGINE 2 BY FOLLOWING CHECKLIST. AFTER ENGINE WASSDR ASAA2021040834532Blade · damagedPER T/C 78472010 # 2 ENG. FAN LUBE #9 PLATFORM ELASTORMER IS TORN ON ONE SIDE. GROUNDED - YES. REF T/C 78472010 # 2 ENG FAN LUBE, #9 PLATFORM REPLACED AND NEW PLATFORM INSTALLED DURING LUBE.SDR ASAA2021040834531Spinner · damagedPER T/C 78472010 #2 ENG. FAN BLADE LUBE FRONT SPINNER CONE MISSING ANODIZED COATING BEYOND LIMITS. GROUNDED - YES. INSTALLED NEW FRONT SPINNER CONE REF B737-800 AMM 72-21-01/401.SDR ASAA2021040534511Spacer · debondedPER T/C 78472010 #1 ENG FAN BLADE LUBE #1,10,13, 16,17,19,20 AND 24 SPACERS ELASTOMERS ARE DISBONDED . GROUNDED - YES. REPLACED SPACERS PER TC# 78472010.SDR UIEA2021040300816Blade · dented#2 ENG HAS ONE FAN BLADE WITH A DENT ON THE LEADING EDGE.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;">CLEANED DENTED AREA OF # 2 ENG FAN BLADE FOUND WITHIN LIMITS AT LEADING EDGE PER B767-300 AMM 72-31-02-226-012-H00. PERFORMED NDT SPOT FLOURESCENT PENETRASDR ASAA2021040234500Blade · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON #1 ENG, T/C #78472010, FOUND ALL SHIMS WITH 25% TO 100% MOLYDAG COATING LOSS. GROUNDED - YES. REPLACED 24 EACH SHIMS DURING THE PERFORMANCE OF T/C 78472010 OF THIS WORK ORDER.SDR ASAA2021040234499Blade · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON #1 ENG. T/C #78472010, FOUND #18 SHIM DAMAGED. GROUNDED - YES. REMOVED AND REPLACED #18 SHIM REF T/C 78472010.SDR UIEA2021040200814Engine · contaminatedDURING W/A FOUND ENG OIL IN THE INLET OF ENG #1(<P>NO OIL SERVICE REQUIRED. PERFORMED SYSTEM CLEANING. #1 ENG RUN UP BY FLIGHT CREW ASSISTANT FOR 5 MIN PER AMM 79-00-00. NO EVIDENCE OF LEAK DETECTED AFTER SHUTDOWN. ALL PARAMETERS NORMAL. AC OK FOR SERVICE. OILSDR ASAA2021032934447Spacer · debondedPER T/C 78472010 # 2 ENG FAN BLADE LUBE SPACERS # 1, 2, 7, 10, AND 17 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED # 2 ENG SPACERS # 1, 2, 7, 10, AND 17 REF TASK CARD 78472010.SDR ASAA2021032934446Blade · wornPER T/C 78472010 # 2 ENG FAN BLADE LUBE # 21 BLADE CU-NI-IN COATING MISSING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED # 2 ENG FAN BLADE # 21, AND ALSO # 9 AS ITS PAIR REF TASK CARD 78472010.SDR ASAA2021032534409Blade · damagedON WALK AROUND FOUND #1 ENGINE, #4 BLADE HAS DISTORTION. GROUNDED - YES. FAN BLADE DAMAGE APPROX .100 FROM BLADE TIP ON LEADING EDGE WAS FOUND TO BE OUT OF LIMITS. ACCOMPLISHED GVI AROUND #1 ENGINE INTAKE AND FAN BLADE IAW B737-900 AMM 72-21-02. NO OTHER DEFECSDR ASAA2021032534408Spacer · debondedPER T/C 78472010 #1 ENG FAN LUBE SPACERS #2,3,5,13,16,20,21,23 AND 24 EALSTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED SPACERS #2,3,5,13,16,20,21,23 AND 24 ON ENG #1 REF TASK CARD 78472010.SDR ICRR202103250001Pin · crackedA CRACK INDICATION WAS DISCOVERED DURING LIQUID PENETRANT INSPECTION PER SPM 70-32-02.SDR ASAA2021031934338Spacer · debondedFOUND ON #2 ENG, REF TC 78472010, 3 QTY SPACERS DUE TO ELASTOMER DIS-BONDING, SPACERS 24, 17, AND 6 NEED REPLACED. GROUNDED - YES. REMOVED AND REPLACED # 24, 17, AND 6 SPACER ON #2 ENG REF TASK CARD 78472010.SDR ASAA2021031734311Blade · damagedPER T/C 78472010 #2 ENG FAN BLADE LUBE, PLATFORMS #15 & 18 ELASTOMERS ARE TORN. GROUNDED - YES. REMOVED AND REPLACED ON #2 ENG PLATFORMS #15 & #18. REF T/C 78472010.SDR ASAA2021031734313Blade · wornPER T/C 78472010 #2 ENG. FAN BLADE LUBE, #17 FAN BLADE MISSING CU-NI-IN COATING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED BLADE #17 AND ITS PAIR #5 ON #2 ENG. REF. T/C 78472010.SDR ASAA2021031734312Spacer · debondedPER T/C 78472010 #2 ENG. FAN BLADE LUBE, SPACER #20 ELASTOMER IS DIDBONDED. GROUNDED - YES. REMOVED AND REPLACED #20 SPACER ON #2 ENG. REF T/C 78472010.SDR AALA202103159028Blade · damagedAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A BIRD STRIKE ON #2 ENGINEAT 300 FEET ON TAKE OFF. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORF WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT: REPLACED #2 ENGINE FAN BLADES #19 SDR ASAA2021030934261Spacer · debondedPER T/C 78472010 #1 ENG. FAN BLADE LUBE, SPACERS #1, 11, 18, AND 22 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REPLACED #1 ENG. FAN BLADE SPACERS #1, 11, 18, AND 22 PER T/C 78472010.SDR ASAA2021030134217Blade · crackedREF T/C # 78472022 SPECIAL DETAILED INSPECTION (SDI) (BOROSCOPE) - CFM56 - 7 ENG HPT BLADES. #1 ENG . S/N 893814. FOUND INTERSECTING CRACK LPT NGV STG - 1 ALONG W/3 FULL CRACKS IN FULLSET, 1 NGV W/HOLE LESS THAN .039 SQ. INCH ". GROUNDED - YES. REMOVED AND REP
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